Detail publikace
Low Cost Fixed Wing UAV for Development of Control Laws
KRAUS, D. NĚMEČEK, J.
Anglický název
Low Cost Fixed Wing UAV for Development of Control Laws
Typ
Stať ve sborníku v databázi WoS či Scopus
Jazyk
en
Originální abstrakt
The project is focused on the development of both simulated and real UAV platform for testing of flight control algorithms. The aim of this paper was to develop a platform that allows initial design of controllers using non-linear and linearized model of UAV in Matlab/Simulink environment. Once the controllers are designed, tuned and verified in simulation, it can then be loaded into low cost UAV platform using automated code generation. The approach was verified on real plane in real environment.
Klíčová slova anglicky
UAV, model based design, navigation
Vydáno
2014-12-03
ISBN
978-80-214-4817-9
Kniha
Mechatronics – Mechatronika (ME), 2014 16th International Conference on
Strany od–do
234–241
Počet stran
8
BIBTEX
@inproceedings{BUT111202,
author="David {Kraus} and Jakub {Němeček}",
title="Low Cost Fixed Wing UAV for Development of Control Laws",
booktitle="Mechatronics - Mechatronika (ME), 2014 16th International Conference on",
year="2014",
pages="234--241",
doi="10.1109/MECHATRONIKA.2014.7018264",
isbn="978-80-214-4817-9"
}